What was found
CORROSION ON EXTERNAL FUSELAGE SKIN BETWEEN BS 640 AND 660, STRINGERS 28L - 28R. REWORKED AREA AND FOUND WITHIN LIMITS IAW SRM 53-00-01, ALLOWABLE DAMAGE 1, DETAIL II, FIG 101, SHEET 4 OF 6.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON EXTERNAL FUSELAGE SKIN BETWEEN BS 640 AND 660, STRINGERS 28L - 28R. REWORKED AREA AND FOUND WITHIN LIMITS IAW SRM 53-00-01, ALLOWABLE DAMAGE 1, DETAIL II, FIG 101, SHEET 4 OF 6.